Can you calculate the nodal forces for my beam with distributed loading?
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Dear Sir/Madam, My name is John Smith, and I am a student at the University of London. I have one assignment to complete, and it involves the analysis of a beam. navigate to this site The loadings to be applied at the ends of the beam are distributed uniformly. The beam is a triangular shaped slender structure, measuring 1.8 meters (L) by 0.6 meter (w) and 0.2 meters (h). The base area is 0.45 square meter. The cross sectional area of the beam is
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I have calculated the nodal forces for a given beam with distributed loading using ABAQUS software. The beam is a rigid circular cylinder of radius 1.0 m and depth 0.2 m. It is subjected to uniformly distributed loads. The total mass of the beam is 12.0 kg. I used ABAQUS to compute the nodal forces in the X, Y, and Z directions. For this, I set up the beam as shown in figure 1, and used the built-in loads (2.0 k
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